K. Tamaki
Papers
2
Total Citations
17
H-Index
2
About
K. Tamaki is a researcher in aerospace and robotic control systems, specializing in the dynamics and near-optimal control of space robots. Their work focuses on the challenging problem of managing three-dimensional attitude maneuvers for multi-body systems—such as those with universal or ball-in-socket joints—that carry initial angular momentum, a critical scenario for free-floating spacecraft. Tamaki’s major contributions include developing nonlinear affine control models for space robots with two rigid bodies and proposing near-optimal control methods that achieve efficient attitude regulation without requiring full optimality. Their most-cited paper, “3D attitude near-optimal control of a universal joint space robot model with initial angular momentum” (2009, 9 citations), introduces a universal joint model and a practical control strategy for nonlinear systems. A follow-up work (2010, 8 citations) extends this approach to ball-in-socket joint models, demonstrating the versatility of their methods. Though their citation counts are modest, Tamaki’s research has provided foundational insights into the control of space robots under realistic initial momentum conditions, making their work valuable for students and engineers in space robotics and nonlinear control theory.
Research Focus
Key Achievements
Top Papers
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